US7716838B2 - Method for manufacturing a bearing ring - Google Patents
Method for manufacturing a bearing ring Download PDFInfo
- Publication number
- US7716838B2 US7716838B2 US11/169,179 US16917905A US7716838B2 US 7716838 B2 US7716838 B2 US 7716838B2 US 16917905 A US16917905 A US 16917905A US 7716838 B2 US7716838 B2 US 7716838B2
- Authority
- US
- United States
- Prior art keywords
- manufacturing
- ring
- raceway surface
- surface formation
- bearing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active, expires
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 32
- 238000000034 method Methods 0.000 title claims description 22
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 44
- 239000000463 material Substances 0.000 claims abstract description 34
- 239000002131 composite material Substances 0.000 claims abstract description 28
- 238000005242 forging Methods 0.000 claims abstract description 26
- 239000000843 powder Substances 0.000 claims abstract description 26
- 229910052751 metal Inorganic materials 0.000 claims abstract description 7
- 239000002184 metal Substances 0.000 claims abstract description 7
- 230000002093 peripheral effect Effects 0.000 claims description 21
- 229910000831 Steel Inorganic materials 0.000 claims description 11
- 239000010959 steel Substances 0.000 claims description 11
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 8
- 229910001141 Ductile iron Inorganic materials 0.000 claims description 5
- 239000000919 ceramic Substances 0.000 claims description 5
- 238000005299 abrasion Methods 0.000 claims description 4
- 238000000748 compression moulding Methods 0.000 claims description 4
- 238000005096 rolling process Methods 0.000 claims description 3
- 238000005245 sintering Methods 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims 2
- 229910045601 alloy Inorganic materials 0.000 claims 2
- 239000000956 alloy Substances 0.000 claims 2
- 229910052782 aluminium Inorganic materials 0.000 claims 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 2
- 239000010936 titanium Substances 0.000 claims 2
- 229910052719 titanium Inorganic materials 0.000 claims 2
- 150000002739 metals Chemical class 0.000 claims 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 abstract description 6
- 229910001092 metal group alloy Inorganic materials 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 5
- 239000003562 lightweight material Substances 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- 238000007789 sealing Methods 0.000 description 2
- 101001139126 Homo sapiens Krueppel-like factor 6 Proteins 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910001234 light alloy Inorganic materials 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C19/00—Bearings with rolling contact, for exclusively rotary movement
- F16C19/22—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings
- F16C19/34—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load
- F16C19/36—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with a single row of rollers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/10—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of articles with cavities or holes, not otherwise provided for in the preceding subgroups
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/08—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/58—Raceways; Race rings
- F16C33/64—Special methods of manufacture
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
- F16H1/32—Toothed gearings for conveying rotary motion with gears having orbital motion in which the central axis of the gearing lies inside the periphery of an orbital gear
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H49/00—Other gearings
- F16H49/001—Wave gearings, e.g. harmonic drive transmissions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/02—Gearboxes; Mounting gearing therein
- F16H57/021—Shaft support structures, e.g. partition walls, bearing eyes, casing walls or covers with bearings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49643—Rotary bearing
- Y10T29/49679—Anti-friction bearing or component thereof
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49643—Rotary bearing
- Y10T29/49679—Anti-friction bearing or component thereof
- Y10T29/49682—Assembling of race and rolling anti-friction members
- Y10T29/49684—Assembling of race and rolling anti-friction members with race making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49643—Rotary bearing
- Y10T29/49679—Anti-friction bearing or component thereof
- Y10T29/49689—Race making
Definitions
- the present invention relates to a method for manufacturing a lightweight bearing ring in which a portion forming a raceway surface of the bearing ring is formed from a ferrous material, and the remaining portion is formed from aluminum alloy or another lightweight material.
- the inner and outer rings of a bearing are manufactured from bearing steel, ductile cast-iron, and other high-density materials in order to maintain abrasion resistance and other properties of a raceway surface of a rolling element.
- a composite bearing ring made of a raceway ring main body member comprised of a light alloy and a raceway surface formation member comprised of a ferrous element is proposed in JP-A 2000-186718 for reducing the weight of the bearing.
- a method for manufacturing this composite bearing ring is proposed in JP-A 2002-339991.
- a main object of the present invention is to provide a method for manufacturing a bearing ring in which a raceway surface formation portion formed from a material which has excellent abrasion resistance is securely and integrally formed with a raceway ring main body portion formed from a lightweight material.
- a configuration may be adopted herein whereby the annular composite member in which the raceway surface formation ring, a preform, and the remaining regions of the raceway ring main body portion are integrally formed by performing powder forging using the powder of the first material in a state in which the raceway ring main body portion is divided into a plurality of regions, at least a portion thereof is preformed using the powder of the first material, and the preform and the raceway surface formation ring are fixed in the forging die.
- preforming an insert during powder forging can be positioned with good precision in any position.
- the annular composite member is preferably manufactured in which the raceway surface formation ring, a first segment, and the remaining regions of the raceway ring main body portion are formed integrally by preforming the first of two segments that include a first and second segment with a shape that is obtained when the raceway ring main body portion is laterally divided in a plane perpendicular to a central axis thereof using the powder of the first material, and performing powder forging using the powder of the first material while the first segment and the raceway surface formation ring are fixed in the forging die.
- a configuration may be adopted wherein the composite member is manufactured in which the raceway surface formation ring and the first and second segments are integrally formed by a process in which both the first and second segments are preformed, and powder forging is performed while the raceway surface formation portion and the first and second segments are fixed in the forging die.
- Aluminum alloy, titanium alloy, and other light metal alloys or ceramics may be used as the first material.
- Bearing steel, die steel, ductile cast-iron, or stainless steel-titanium alloy may be used as the second material.
- the present invention relates to a bearing ring whose distinguishing feature is that it is manufactured by the method described above.
- a raceway ring main body portion and a raceway surface formation portion comprised of different materials are integrally formed by powder forging.
- FIG. 1 is a schematic cross-sectional diagram of a silk hat shaped wave gear device unit according to the present invention
- a wave gear device unit according to the present invention will be described hereinafter with reference to the drawings.
- FIG. 1 is a cross-sectional diagram of a wave gear device unit provided with a silk hat shaped wave gear device into which a lightweight cross roller bearing manufactured according to the present invention is incorporated.
- FIG. 2 is a diagram showing a structure of the silk hat shaped wave gear device.
- a wave gear device unit 1 has a first end plate 2 and a second end plate 3 positioned with a fixed gap between the same in a direction of a unit axis line 1 a , and a cross roller bearing 4 positioned between the first and second end plates 2 and 3 .
- a silk hat shaped wave gear device 5 is built into a unit housing comprised of the first and second end plates 2 and 3 and an outer ring 41 of the cross roller bearing 4 .
- a shaft hole is formed in a center of the first and second end plates 2 and 3 , and a hollow input shaft 8 rotatably supported by ball bearings 6 and 7 is passed through the shaft hole.
- the cross roller bearing 4 is provided with the outer ring 41 and an inner ring 42 , and a plurality of rollers 43 inserted into an annular raceway formed in compartmental fashion between the inner and outer rings.
- the outer ring 41 is a composite component provided with an annular outer ring main body portion 411 and an annular raceway surface formation portion 412 that is formed integrally with an inner peripheral surface of the outer ring main body portion and has a raceway surface formed on an inner peripheral surface thereof.
- raceway surface formation rings 412 and 422 are covered on their opposite and axially outwardly facing sides by the respective outer ring main body portions 411 and 421 .
- the inner ring 42 is a composite component provided with an annular shaped wide inner ring main body portion 421 and an annular raceway surface formation portion 422 that is formed integrally with an outer peripheral surface portion on a side of one end of the inner ring main body portion 421 and has a raceway surface formed on an outer peripheral surface thereof.
- raceway surface formation rings 412 and 422 are covered on their opposite and axially outwardly facing sides by the respective outer ring main body portions 411 and 421 .
- the inner ring 42 in this arrangement is provided with an annular toothed portion 512 that is formed integrally with an inner peripheral surface portion on a side of the other end of the inner ring main body portion 421 and has an inner tooth 511 formed in an inner peripheral surface thereof.
- the inner ring 42 in the present example is a component that also acts as a rigid internal gear of the silk hat shaped wave gear device 5 described hereinafter.
- the inner ring main body portion 421 of the inner ring 42 thus configured is fixedly fastened to the second end plate 3 by a tightening bolt not shown in the drawing.
- the silk hat shaped wave gear device 5 is provided with an annular rigid internal gear 51 , a silk hat shaped flexible external gear 52 , and a wave generator 53 having an elliptical profile.
- the rigid internal gear 51 is formed integrally with the inner ring 42 of the cross roller bearing 4 , as described above.
- the annular toothed portion 512 in which the inner tooth 511 is formed in the inner peripheral surface thereof is formed integrally with the inner peripheral surface of the inner ring 42 , which doubles as the internal gear.
- the flexible external gear 52 is provided with a cylindrical body 521 , an annular diaphragm 522 formed continuously with one end of the cylindrical body to extend radially outward, a thick annular boss 523 formed continuously with an outer peripheral edge of the diaphragm 522 , and an external tooth 524 formed on an outer peripheral surface of the other end portion of the cylindrical body 521 , and has a silk hat shape overall.
- the annular boss 523 is disposed between an annular end surface of the outer ring 41 of the cross roller bearing 4 and the first end plate 2 , and is fixedly fastened to these components by a tightening bolt (not shown in the drawing). Consequently, the flexible external gear 52 and the rigid internal gear 51 can rotate relative to each other via the cross roller bearing 4 .
- the wave generator 53 is provided with an elliptically profiled rigid cam plate portion 531 formed on an outer peripheral surface of the input shaft 8 , and a ball bearing 532 , and this ball bearing 532 is fitted between an outer peripheral surface of the rigid cam plate portion 531 and an inner peripheral surface of a portion in which the external teeth 524 of the flexible external gear 52 are formed.
- An annular plate 9 for forming a bolt flange is attached to an annular end surface 415 of the outer ring main body portion in which a bolt hole 414 formed in the outer ring main body portion 411 of the outer ring 41 opens, and this annular plate 9 is also fixedly fastened on a side of the outer ring main body portion 411 by a tightening bolt.
- a sealing ring 91 used as an oil seal is attached to a portion of the annular plate 9 on an internal peripheral edge side thereof, and a gap between the outer ring 41 and the inner ring 42 is sealed by this sealing ring 91 .
- a portion of the rotational input shaft 8 that protrudes from the second end plate 3 is connected and fixed to a motor output shaft or other rotation source.
- the first end plate 2 or second end plate 3 is also connected and fixed on a load side.
- This rotation is significantly reduced in speed compared with an input rotational speed. Since one of the first end plate 2 and second end plate 3 is connected to the load side, and the other is fixed so as not to rotate, reduced rotation is outputted and transmitted to the load side from the side of the end plate connected to the load side.
- the outer ring 41 of the cross roller bearing 4 is the composite component comprised of the outer ring main body portion 411 and the raceway surface formation portion 412 .
- the inner ring 42 is the composite component comprised of the inner ring main body portion 421 , the raceway surface formation portion 422 , and the toothed portion 512 in which internal teeth 511 are formed in the inner peripheral surface thereof.
- the outer ring main body portion 411 and the inner ring main body portion 421 are formed from a lightweight material (first material) that is lighter than a ferrous material, and ceramics or a light metal alloy such as an aluminum alloy or titanium alloy, for example, may be used therein.
- first material a lightweight material
- ceramics or a light metal alloy such as an aluminum alloy or titanium alloy, for example
- the raceway surface formation portions 412 and 422 in which the raceway surface is formed, and the toothed portion 512 in which internal teeth are formed are formed from of a ferrous material or other commonly used material (second material).
- second material commonly used material
- bearing steel, die steel, ductile cast-iron, stainless-steel-titanium alloy, and the like can be used to form these components.
- the input shaft 8 is also formed from aluminum alloy, titanium alloy, or another light metal alloy, or from plastic, a ceramic, or another lightweight material, and the rigid cam plate portion 531 of the wave generator 53 formed on the outer peripheral surface thereof is also formed from the same lightweight material.
- a raceway surface formation ring 412 A for forming the raceway surface formation portion 412 is manufactured from bearing steel, die steel, stainless steel-titanium alloy, or another second material (step ST 1 ).
- One or more types of starting material powder are admixed/mixed, and a metal powder (first material powder) is prepared for manufacturing the outer ring main body portion 411 (step ST 2 ).
- Powder forging using the metal powder is then performed in a state in which the raceway surface formation ring 412 A is inserted into a forging die (step ST 3 ).
- a composite component 41 A used for the outer ring is obtained in which a ring-shaped portion 411 A for forming the outer ring main body portion 411 on an outer peripheral side of the raceway surface formation ring 412 A is integrally formed.
- step ST 4 Sizing or another after-treatment is performed for this composite component 41 A (step ST 4 ), and the outer ring 41 is obtained.
- the outer ring main body portion 411 may be preformed prior to powder forging in this arrangement.
- first and second segments 411 a and 411 b having a shape that is obtained when the outer ring main body portion 411 is laterally divided in a plane perpendicular to a central axis thereof may be preformed in advance by compression molding, or by compression molding and heating/sintering (steps ST 11 and ST 12 ).
- the raceway surface formation ring 412 A, and the segments 411 a and 411 b are mounted in the forging die, and powder forging is performed (step ST 3 ).
- a composite component 41 B is obtained in which the segments 411 a and 411 b are integrally formed into a ring-shaped portion 411 A corresponding to the outer ring main body portion 411 , while at the same time, the ring-shaped portion 411 A and the raceway surface formation ring 412 A are integrally formed.
- a prescribed after-treatment is performed for this composite component 41 B (step ST 4 ), and the outer ring 41 is obtained.
- Only one of the first and second segments 411 a and 411 b may be preformed in advance.
- the first segment 411 a is preformed in advance (step ST 11 ), and powder forging is performed using the metal powder while this first segment and the raceway surface formation ring 412 A are mounted in the forging die (step ST 3 ).
- a composite component 41 C is obtained in which the raceway surface formation ring 412 A and the ring-shaped portion 411 A corresponding to the outer ring main body portion 411 are integrally formed, and the outer ring 41 is obtained by performing an after-treatment on the composite component 41 C (step ST 4 ).
- the inner ring 42 may be manufactured in the same manner.
- the raceway surface formation portion 422 and the toothed portion 512 are formed in advance from a ferrous material, and powder forging is performed using metal powder while these members are mounted in the forging die, whereby a composite component can be obtained in which the raceway surface formation portion 422 and toothed portion 512 are integrally formed with the inner ring main body portion 421 .
- the inner ring 42 is obtained by performing machining or the like to form inner teeth in the composite component.
- the present invention was applied to a cross roller bearing in the example described above, but it is apparent that the present invention may also be applied in the same manner to a ball bearing or other type of bearing.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Materials Engineering (AREA)
- Rolling Contact Bearings (AREA)
- Forging (AREA)
Abstract
Description
Claims (11)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2004195634A JP4363523B2 (en) | 2004-07-01 | 2004-07-01 | Manufacturing method of bearing race |
| JP2004-195634 | 2004-07-01 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20060000096A1 US20060000096A1 (en) | 2006-01-05 |
| US7716838B2 true US7716838B2 (en) | 2010-05-18 |
Family
ID=34937655
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/169,179 Active 2029-03-18 US7716838B2 (en) | 2004-07-01 | 2005-06-28 | Method for manufacturing a bearing ring |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7716838B2 (en) |
| EP (1) | EP1612454B1 (en) |
| JP (1) | JP4363523B2 (en) |
| DE (1) | DE602005012558D1 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180031108A1 (en) * | 2016-07-29 | 2018-02-01 | Seiko Epson Corporation | Robot and gear device |
| US20180162524A1 (en) * | 2016-12-11 | 2018-06-14 | Bell Helicopter Textron, Inc. | Gear Shaft for Accommodating Thermal Expansion and Transmission System Incorporating the Same |
| US10077829B2 (en) | 2012-08-21 | 2018-09-18 | Nexen Group, Inc. | Strain wave gear system |
| US11174929B2 (en) | 2012-08-21 | 2021-11-16 | Nexen Group, Inc. | Strain wave gear system |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102954190B (en) * | 2011-08-19 | 2015-09-09 | 鸿富锦精密工业(深圳)有限公司 | Speed reducer |
| JP5496426B1 (en) * | 2012-12-12 | 2014-05-21 | 株式会社ハーモニック・ドライブ・システムズ | Wave gear unit with input bearing |
| CN106104076B (en) * | 2014-03-31 | 2018-07-06 | 谐波传动系统有限公司 | The manufacturing method of Wave gear device and multilayer hollow body |
| FR3105319B1 (en) * | 2019-12-20 | 2022-03-18 | Skf Aerospace France | Ring for connecting element, connecting element and corresponding method of manufacture |
| CN112024806A (en) * | 2020-06-10 | 2020-12-04 | 黄石哈特贝尔精密锻造有限公司 | Plane thrust ball bearing ring integrated forging forming die |
| CN113894291B (en) * | 2021-09-23 | 2022-07-26 | 石家庄铁道大学 | Method for melting GCr15 bearing steel for high-speed rail in selective laser zone |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB570141A (en) | 1942-05-12 | 1945-06-25 | George Haywood Kendall | Improvements in or relating to anti-friction bearings |
| GB601973A (en) | 1945-02-01 | 1948-05-18 | George Hayward Kendall | Improvements in or relating to anti-friction bearings |
| US3666456A (en) | 1969-08-04 | 1972-05-30 | Federal Mogul Corp | Method of making composite wear resistant articles,such as face seals |
| US3727999A (en) | 1972-03-20 | 1973-04-17 | W Dunn | Composite heavy-duty bearing race |
| US3770332A (en) | 1971-06-14 | 1973-11-06 | Federal Mogul Corp | Composite heavy-duty bushing and method of making the same |
| US3772935A (en) | 1972-03-20 | 1973-11-20 | W Dunn | Composite heavy-duty sintered powdered machine element |
| US4145798A (en) | 1977-10-21 | 1979-03-27 | Federal-Mogul Corporation | Forging recessed configurations on a body member |
| US4343072A (en) * | 1978-09-25 | 1982-08-10 | Societe Nouvelle De Roulements | Method of manufacturing composite rings for bearings |
| EP0278682A2 (en) | 1987-02-06 | 1988-08-17 | The Timken Company | Powder metal composite and method of its manufacture |
| EP0623761A1 (en) | 1993-03-10 | 1994-11-09 | Bayerische Motoren Werke Aktiengesellschaft | Shaft bearing in an engine block, especially connecting rod in the drive unit of an internal combustion engine |
| US6045750A (en) | 1997-10-14 | 2000-04-04 | Camco International Inc. | Rock bit hardmetal overlay and proces of manufacture |
| JP2000186718A (en) | 1998-12-22 | 2000-07-04 | Harmonic Drive Syst Ind Co Ltd | Cross roller bearing and wave gear unit |
| JP2002339991A (en) | 2001-05-22 | 2002-11-27 | Harmonic Drive Syst Ind Co Ltd | Manufacturing method of lightweight bearing |
-
2004
- 2004-07-01 JP JP2004195634A patent/JP4363523B2/en not_active Expired - Lifetime
-
2005
- 2005-06-24 EP EP05013707A patent/EP1612454B1/en not_active Expired - Lifetime
- 2005-06-24 DE DE602005012558T patent/DE602005012558D1/en not_active Expired - Lifetime
- 2005-06-28 US US11/169,179 patent/US7716838B2/en active Active
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB570141A (en) | 1942-05-12 | 1945-06-25 | George Haywood Kendall | Improvements in or relating to anti-friction bearings |
| GB601973A (en) | 1945-02-01 | 1948-05-18 | George Hayward Kendall | Improvements in or relating to anti-friction bearings |
| US3666456A (en) | 1969-08-04 | 1972-05-30 | Federal Mogul Corp | Method of making composite wear resistant articles,such as face seals |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10077829B2 (en) | 2012-08-21 | 2018-09-18 | Nexen Group, Inc. | Strain wave gear system |
| US11174929B2 (en) | 2012-08-21 | 2021-11-16 | Nexen Group, Inc. | Strain wave gear system |
| US11852229B2 (en) | 2012-08-21 | 2023-12-26 | Nexen Group, Inc. | Strain wave gear system |
| US20180031108A1 (en) * | 2016-07-29 | 2018-02-01 | Seiko Epson Corporation | Robot and gear device |
| US10451174B2 (en) * | 2016-07-29 | 2019-10-22 | Seiko Epson Corporation | Robot and gear device |
| US20180162524A1 (en) * | 2016-12-11 | 2018-06-14 | Bell Helicopter Textron, Inc. | Gear Shaft for Accommodating Thermal Expansion and Transmission System Incorporating the Same |
| US10526081B2 (en) * | 2016-12-11 | 2020-01-07 | Textron Innovations Inc. | Gear shaft for accommodating thermal expansion and transmission system incorporating the same |
Also Published As
| Publication number | Publication date |
|---|---|
| JP4363523B2 (en) | 2009-11-11 |
| JP2006017222A (en) | 2006-01-19 |
| US20060000096A1 (en) | 2006-01-05 |
| DE602005012558D1 (en) | 2009-03-19 |
| EP1612454A1 (en) | 2006-01-04 |
| EP1612454B1 (en) | 2009-01-28 |
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